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镍基高温合金的热机械疲劳寿命预测模型研究

崔海涛 钱春华

中国机械工程2024,Vol.35Issue(1):67-73,82,8.
中国机械工程2024,Vol.35Issue(1):67-73,82,8.DOI:10.3969/j.issn.1004-132X.2024.01.006

镍基高温合金的热机械疲劳寿命预测模型研究

Research on Thermo-mechanical Fatigue Life Prediction Model of Ni-base Superalloy

崔海涛 1钱春华1

作者信息

  • 1. 南京航空航天大学能源与动力学院,南京,210016
  • 折叠

摘要

Abstract

In phase TMF tests on nickel-based high-temperature alloy GH4169,a commonly used material for engine hot end components,under conditions of 200-450 ℃ and 400-650 ℃ is conduc-ted.Considering the micro damage strain energy of polycrystalline materials in the elastic stages under the condition of TMF,a TMF life prediction model suitable for polycrystalline materials was pro-posed,model parameters were determined by combining the TMF test data.Three superalloys,GH4169,IN718,DD8,were used to evaluate the TMF life prediction ability of this model.The pre-diction accuracy of the life model is higher than that of the Manson-Coffin model and Ostergen model commonly used for TMF life prediction.

关键词

镍基高温合金/热机械疲劳(TMF)/损伤应变能/寿命预测

Key words

nickel-base superalloy/thermo-mechanical fatigue(TMF)/dmamage strain energy/life prediction

分类

航空航天

引用本文复制引用

崔海涛,钱春华..镍基高温合金的热机械疲劳寿命预测模型研究[J].中国机械工程,2024,35(1):67-73,82,8.

基金项目

国家自然科学基金(91860111) (91860111)

中国机械工程

OA北大核心CSTPCD

1004-132X

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